US2485522A - Humidity control in aircraft air conditioning - Google Patents

Humidity control in aircraft air conditioning Download PDF

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US2485522A
US2485522A US614323A US61432345A US2485522A US 2485522 A US2485522 A US 2485522A US 614323 A US614323 A US 614323A US 61432345 A US61432345 A US 61432345A US 2485522 A US2485522 A US 2485522A
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air
cabin
flow
humidity
reexpanded
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US614323A
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Soren K Andersen
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Garrett Corp
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Garrett Corp Aires Mfg Company
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
    • B64D2013/0603—Environmental Control Systems
    • B64D2013/0688—Environmental Control Systems with means for recirculating cabin air

Definitions

  • My invention relates to air conditioning systems for aircraft and relates in particular to an air conditioning system which embraces the economics resulting from the use of expansion turbines in the cooling of air delivered into or circulatedthrough aircraft cabins, and which exercises a control over the humidity of the air without necessity of replacing or adding moisture to make up for the excess removal of water from the air occurring where an expansion turbine is employed as a means for reducing the temperature of and recovering power from a flow of air in an air cooling system.
  • this invention the cooled and humidity-adjusted air from the humidity con-.
  • trol unit is intermixed with the main volume of air which is flowing toward the cabin and constitutes a means for regulating the humidity of this main flow of air, in accordance with the cabin requirements.
  • a further object of the-invention is to provide'55 2 a humidity control unit having therein a proportioning valve for diverting a proportion of the cooled air through the water removal zone of the humidity control unit, this proportioning valve being actuated. in accordance with the needs of the cabin interior determined by a humidostat which controls the action of a motor or motivating means connected to the proportioning valve so as to move it into its different positions -of air-flow regulation.
  • I show an aircraft cabin III which receives a flow of air from a main air duct ll.
  • cabin is used in the broad sense or meaning of a space or compartment which is air-conditioned. Circulation of air through the cabin is accomplished by release of air from the opposite end of the cabin i0 through an outlet duct I2 leading to the intake of a blower I3, the outlet of which blower i3 is connected by a duct M with the main air duct i 8, thereby forming a cabin air recirculating system.
  • a replenishment blower or air compressor 25 is provided for delivery of replenishment air into the cabin.
  • This blower or compressor i5 is shown connected to the duct M.
  • the quantity of air pumped by the device i5 will, of course, depend upon the pressure conditions required in the aircraft cabin ID. If the aircraft is being flown at levels below the altitude requiring pressurization, the blower l5 will serve merely as a means for adding to the'cabin air only a sufficient volume of air to accomplish oxygen replacement, but if pressurization of the cabin I0 is required, the blower l5 will be required to feed suflicient air under pressure into the system to maintain required pressure in the cabin.
  • the outlet of the cooler 20 is connected through a duct 2
  • the diagrammatically shown cooler 20 may be any of the known devices for extracting heat from a fiow of air. Accordingly, it will be recognized that this cooler 20 may be a heat exchanger or a part of a mechanical refrigerating system employing a condensible refrigerant.
  • the cooler 20 is controlled in accordance with changes in temperature in the cabin by control means of any of the known types, including a thermostat 21 having operative connection with the cooler 20 as diagrammatically indicated at 28.
  • the humidity control unit 24 includes a shell 29 forming a chamber 30. At the forward end of this chamber 30 there is a flow directing and proportioning valve 3
  • is shown in an intermediate position so as to divide the flow of cold air from the duct 23 into an upper path of flow and a lower path of flow indicated respectively by arrows 35 and 35'.
  • the lower path of flow 35' is through a moisture removal zone comprising a filter 36 having therein means for causing condensation of moisture from the fiow of cold air which passes therethrough, such means being shown as a mass of fibers or filamentous material 31 forming a myriad of tortuous passages and a large surface area exposed'to the flow of moisture laden cold air.
  • the moisture entrained in the air as it leaves the expansion turbine 22 consists of very fine globules which, if maintained at the small size in which they are formed in the outlet of the turbine 4 22, will remain in suspension as the air flows through a duct substantially without turbulence.
  • has a lever 40 fixed thereon connected through a link 4
  • the motor mechanism 42 is controlled by a humidostat 43 situated within the cabin Hi, this humidostat 43 having operative connection with the motor mechanism 42 as indicated diagrammatically by the line 44.
  • the humidostat control of the reversible motor mechanism 42 is indicated only diagrammatically for the reason that this part of the applicants system follows prior art practices such, for example, as shown in the abandoned application of William G. Rommel, Serial No. 547,269, filed July 29, 1944, for Humidity indicator and control.
  • the rotors of the compressor I and the reexpansion turbine 22 are interconnected by shaft means 46 whereby power recovered by the reexpansion of air in the turbine 22' iscarried back to the compressor thereby reducing the load on the motor 41 which is shown driving the shaft 46 through bevel gearing 48.
  • a comparatively small flow of air as compared to the main flow of air into the cabin through the duct II is compressed to whatever extent may be required and is passed through the .cooler wherein a thermostat controlled quantity of heat is abstracted therefrom.
  • the reexpansionof the cooled. compressed air through the reexpansion turbine 22 brings the temperature of the air to a low value and reduces the moisture in the air to extremely fine globules which remain in suspension in the air.
  • Under control of the humidostat 43 and the motor mechanism 42, the proportioning valve 3
  • may be positioned as indicated by dotted lines 3
  • the cooled and humidity regulated air modulates the temperature and humidity of the entire volume of the air flowing into the cabin, whereby 0 the temperature and humidity of the air in the cabin are maintained within a predetermined range of values.
  • a cabin air conditioning system of the character described, the combination of: means for recirculating a main flow'of cabin air; means for diverting and compresing a part of said main flow of air; a cooling means; means for passing the diverted compressed air through said cooling means to cool the same; means for reexpanding and further cooling the compressed, cooled air; means for removing moisture from only a part of the reexpanded air; and means for delivering said part of the air back into said main flow of air.
  • a cabin air conditioning system of the character described, the combination of: means for recirculating a main flow of cabin air; means for diverting and compressing a part of said main flow of air; a cooling means; means for passing the diverted compressed air through said cooling means to cool the same; means for reexpanding and further cooling the compressed, cooled air; and a humidity control unit receiving the reexpanded and cooled air, said unit having two paths of flow for the air leading back into said mainflow of air, one of said paths of flow having moisture removing means therein, and a proportioning valve for directing said reexpanded air through said paths of flow, and means responsive to the humidity of the cabin air for controlling said valve, whereby moisture will be'removed from only a portion of said reexpanded air in accordance with the deviation acaaaaa scribed range.
  • a cabin air conditioning system of the I character described the combination of: means for recirculating a main now of cabin air; means for diverting and compressing a ⁇ part of said main flow of air; a cooling mea'ns; means for passing the' diverted compressed air through said cooling means to cool the same; mean for reexpanding and further cooling the compressed, cooled air; means operating in response to changes in temperature of the cabin air for controlling the action of said cooling means; means for removing moisture from only apart of the reexpanded air; and means for delivering said part of the air back into-said main flow of air.
  • a cabin air conditioning system of the character described, the combination of: means for recirculating a main flow of cabin air; means for diverting and compressing a part of said main flow of air; a cooling means; means for passing the diverted compressed air through said cooling means to cool the same; means operating in response to changes in temperature of the cabin air for controlling the action of said cooling means; means for reexpanding and further cooling the compressed, cooled air; and a humidity control unit receiving the reexpanded and cooled air, said unit having two paths of flow for the air leading back into said main flow of air, one of said paths of flow having moisture removing means therein, and a proportioning valve for directing said reexpanded air through said paths of flow, and means responsive to the humidity of the cabin air for controlling said valve, whereby moisture will be removed from only a portion of said reexpanded air in accordance with the deviation of the humidity of the cabin air from a prescribed range.
  • a cabin air conditioning-system of the character described, the combination of: means for recirculating a main flow of cabin air; means for diverting and compressing a part of said main flow of air; a cooling means; means for passing the diverted compressed air through said cooling means to cool the same; means operating in response to changes in temperature of the cabin air for controlling the action of said cooling means; means for reexpanding and fur ther cooling the compressed, cooled air; and a humidity control unit receiving the reexpanded and cooled air, said unit having two paths of fiow for the air leading back into said main flow.
  • one of said paths of flow having moisture removing means therein, a proportioning valve for directing said reexpanded air through said paths of flow, and means responding to changes in the humidity of the cabin air for adjusting the position of said proportioning valve, whereby moisture will be removed from only a portion of said reexpanded air in accordance with the deviation of the humidity of the cabin air from a prescribed range.
  • a cabin air conditioning system of the character described, the combination of means for recirculating a main flow of cabin air; means for diverting and compressing a part of said main flow of air; a cooling means; means for passing the diverted compressed air through said cooling means to cool the same; means for reexpanding and further cooling the compressed, cooled air; and a humidity control unit receiving the reexpanded and cooled air, said unit having two paths of new for the air leading back into said main flow of air, one of said paths of flow having moisture removing means therein,
  • flowstraightening means at least in the outlet I part of said unit, and a proportioning valve for directing said reexpanded air through said paths of flow, and means responsive to the humidity of the cabin air for controlling said valve, whereby moisture will be removed from only a portion of said reexpanded air in accordance with the deviation of the humidity of the cabin'air' from a prescribed range.
  • a cabin air conditioning system having means for circulatingair
  • a humidity control unit receiving the reexpanded and cooled air, said unit having two paths of flow for the air leading into said main flow of air, one of said paths of flow having moisture removing means therein, and a proportioning valve for directing said reexpanded air through said paths of flow,
  • a humidostat for controlling said valve, whereby 9.
  • a cabin air conditioning system of the character described the combination of means for passing a main flow of air into the cabin; means for compressing a second fiow of air; a cooling means; means for passing the compressed air through said coolin means to cool the same;
  • a humidity control unit receiving the reexpanded and cooled air, said unit having two paths of flow for the air leading into said main flow of air, one of said paths of flow having moisture removing means therein, a
  • proportioning valve for directing said reexpanded air through said paths of flow, and means responding to changes in the humidity of the cabin air for adjusting the position of said proportioning valve, whereby moisture will be removed from only a portion of said reexpanded air in accordance with the deviation of the humidity of the cabin air from a prescribed range.
  • a cabin air conditioning system of the -character described the combination of means paths of flow for the air leading into said main flow of air, one of said paths of flow having moisture removing means therein, and a proportioning valve for directing said reexpanded air through said paths of flow, and means responsive to the humidity of the cabin air for controlling said valve, whereby moisture will be removed from only a portion of said reexpanded air in accordance with the deviation of the humidity of the cabin air from a prescribed range.
  • a cabin air conditioning system of the character described, the combination of: means for passing a flow of air into the cabin; means for compressing said flow of air; a cooling means; means for passing the compressed air through said cooling means to cool the same; means for reexpanding and further cooling the compressed cooled air; and a humidity contro1 unit receiv-; ing the reexpanded and cooled air, said unit having two paths of flow for the air leading toward the cabin, one of said paths of flow having mois ture removing means therein, a proportioning valve for directing said reexpanded air through said paths of flow, and means responding to changes in the humidity of the cabin air for adjusting the position of said proportioning valve, whereby moisture will be removed from only a portion of said reexpanded air in accordance with the deviations of the humidity of the cabin air from a prescribed range.
  • a cabin air conditioning system of the character described, the'combination of: means for passing a flow of air into the cabin; means for compressing said flow of air; a cooling means; means for passing the compressed air through said cooling means to cool the same; means operating in response to changes in temperature of the cabin air for controlling the action of said cooling means; means for reexpanding and fur- .ther cooling the compressed cooled air; and a humidity control unit receiving the reexpanded and cooled air, said unit having two paths of HOW for the air leading toward the cabin, one of said paths of flow having moisture removing means therein, a proportioning valve for directing said reexpanded air through said paths or flow.
  • a cabin air conditioning system having means for circulating air

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  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Pulmonology (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Air Conditioning Control Device (AREA)

Description

Oct. 18 1949.
R CONDITIONING S. K. ANDERSEN HUMIDITY common IN AIRCRAFT AI Filed Sept. 4, 1945 INVENTOR- ANDERSE'N SOREN K.
' ATTORNEY Patented Oct. 18,
HUMIDITY CONTROL IN AIRCRAFT AIR CONDITIONING Soren K. Andersen, Los Angeles, Calif., assignor to TheGarrett Corporation, Airesearch Manufactoring Company Division,
Los Angeles,
Calif a corporation of California Application September 4, 1945, Serial No. 614,323
13 Claims.
My invention relates to air conditioning systems for aircraft and relates in particular to an air conditioning system which embraces the economics resulting from the use of expansion turbines in the cooling of air delivered into or circulatedthrough aircraft cabins, and which exercises a control over the humidity of the air without necessity of replacing or adding moisture to make up for the excess removal of water from the air occurring where an expansion turbine is employed as a means for reducing the temperature of and recovering power from a flow of air in an air cooling system.
It is'an object of the invention to provide an air conditioning system for use in aircraft which is comparatively economical and light in weight so that it can be used in aircraft, wherein a relatively small portion of the total volume of the air circulated through or delivered into the cabin is cooled to a comparatively low temperature, partly de-humidified and then mixed with the balance of the air which is flowing as a strea toward the cabin interior.
It is an object of the invention to provide an air conditioning system of the above character having simple means for removing only a controlled portion of the moisture from the relature in the main air duct of the air conditioning system at a minimum.
It is an object of the invention to provide a method and apparatus wherein the cooled air is conducted into a humidity control 'unithaving therein a moisture removing element and means for diverting a portion of the cooled air through the moisture removing element so that moisture will be extracted from a portion of the air determined by the humidity of the air in the aircraft cabin, this humidity control unit having means for minimizing the condensation of moisture from the remaining or undiverted portion of the cooled air. In this invention the cooled and humidity-adjusted air from the humidity con-.
trol unit is intermixed with the main volume of air which is flowing toward the cabin and constitutes a means for regulating the humidity of this main flow of air, in accordance with the cabin requirements.
A further object of the-invention is to provide'55 2 a humidity control unit having therein a proportioning valve for diverting a proportion of the cooled air through the water removal zone of the humidity control unit, this proportioning valve being actuated. in accordance with the needs of the cabin interior determined by a humidostat which controls the action of a motor or motivating means connected to the proportioning valve so as to move it into its different positions -of air-flow regulation.
Further objects and advantages of the invention will be brought out in the following part of the specification.
In the drawing which is schematic in character and for illustrative purposes only, I show an aircraft cabin III which receives a flow of air from a main air duct ll. Herein the term cabin is used in the broad sense or meaning of a space or compartment which is air-conditioned. Circulation of air through the cabin is accomplished by release of air from the opposite end of the cabin i0 through an outlet duct I2 leading to the intake of a blower I3, the outlet of which blower i3 is connected by a duct M with the main air duct i 8, thereby forming a cabin air recirculating system. A replenishment blower or air compressor 25 is provided for delivery of replenishment air into the cabin. This blower or compressor i5 is shown connected to the duct M. The quantity of air pumped by the device i5 will, of course, depend upon the pressure conditions required in the aircraft cabin ID. If the aircraft is being flown at levels below the altitude requiring pressurization, the blower l5 will serve merely as a means for adding to the'cabin air only a sufficient volume of air to accomplish oxygen replacement, but if pressurization of the cabin I0 is required, the blower l5 will be required to feed suflicient air under pressure into the system to maintain required pressure in the cabin.
A portion of the air which is flowing from the blower I3 toward the air inlet I 6 by which the duct II is connected to the cabin interior, is diverted through an air cooling and humidity regulating system S which comprises a compressor or blower l1 having its inlet connected through a duct l8 with the conduit l4, and having its outlet connected through a duct IS with a cooler 20. The outlet of the cooler 20 is connected through a duct 2| with the inlet of an expansion turbine 22 through which the air compressed by the blower and cooled by the cooler 20 is further cooled and reexpanded into a duct 23 which leads to a humidity control unit24 having an outlet 25 connected with the main air duct so that the cooled and humidity regulated air which is passed through the system S may be added to the comparatively large flow of air through the duct l l.
The diagrammatically shown cooler 20 may be any of the known devices for extracting heat from a fiow of air. Accordingly, it will be recognized that this cooler 20 may be a heat exchanger or a part of a mechanical refrigerating system employing a condensible refrigerant. The cooler 20 is controlled in accordance with changes in temperature in the cabin by control means of any of the known types, including a thermostat 21 having operative connection with the cooler 20 as diagrammatically indicated at 28. The humidity control unit 24 includes a shell 29 forming a chamber 30. At the forward end of this chamber 30 there is a flow directing and proportioning valve 3| comprising upper and lower walls 32 and 33 which are connected to a transverse v shaft 34 in such positions that they extend from the shaft 34 at substantially right angles.
The proportioning valve 3| is shown in an intermediate position so as to divide the flow of cold air from the duct 23 into an upper path of flow and a lower path of flow indicated respectively by arrows 35 and 35'. The lower path of flow 35' is through a moisture removal zone comprising a filter 36 having therein means for causing condensation of moisture from the fiow of cold air which passes therethrough, such means being shown as a mass of fibers or filamentous material 31 forming a myriad of tortuous passages and a large surface area exposed'to the flow of moisture laden cold air.
The moisture entrained in the air as it leaves the expansion turbine 22 consists of very fine globules which, if maintained at the small size in which they are formed in the outlet of the turbine 4 22, will remain in suspension as the air flows through a duct substantially without turbulence. So as to minimize turbulence of the air stream as it leaves the humidity control unit 24, thereby minimizing the coalescence of these small moisture globules which will causes them to coalesce into droplets or drops of water, I provide in the humidity control unit 24 and particularly in the outlet portion thereof flow straightening means 38 comprising parallel walls forming parallel passages through which the air passes in such a manner as to minimize turbulent fiow in the air and thereby minimize contact or collision between the minute moisture globules.
The shaft 34 of the flow proportioner 3| has a lever 40 fixed thereon connected through a link 4| with a reversible motor mechanism 42 for swinging the flow proportioner 3| through its various positions. The motor mechanism 42 is controlled by a humidostat 43 situated within the cabin Hi, this humidostat 43 having operative connection with the motor mechanism 42 as indicated diagrammatically by the line 44. The humidostat control of the reversible motor mechanism 42 is indicated only diagrammatically for the reason that this part of the applicants system follows prior art practices such, for example, as shown in the abandoned application of William G. Rommel, Serial No. 547,269, filed July 29, 1944, for Humidity indicator and control.
The rotors of the compressor I and the reexpansion turbine 22 are interconnected by shaft means 46 whereby power recovered by the reexpansion of air in the turbine 22' iscarried back to the compressor thereby reducing the load on the motor 41 which is shown driving the shaft 46 through bevel gearing 48.
In the operation of the invention a comparatively small flow of air, as compared to the main flow of air into the cabin through the duct II is compressed to whatever extent may be required and is passed through the .cooler wherein a thermostat controlled quantity of heat is abstracted therefrom. The reexpansionof the cooled. compressed air through the reexpansion turbine 22 brings the temperature of the air to a low value and reduces the moisture in the air to extremely fine globules which remain in suspension in the air. Under control of the humidostat 43 and the motor mechanism 42, the proportioning valve 3| is moved into its required position. If the humidity of the air in the cabin is above a preselected value, a corresponding proportion of the air will be passed through the moisture removal zone of the humidity control unit represented by the filter 36. It will be understood that under control of the humidostat 43, the proportioning valve 3| may be positioned as indicated by dotted lines 3| so that the entire flow of cooled air follows the path indicated by the arrows 35, no moisture being then removed from the air, except such small amount as may condense on the surfaces of the walls of the humidity control unit 24. Under ordinary conditions of operation, the proportioning valve 3| is maintained in an intermediate position such as that in which it is shown in full lines. However, there may be times when the great humidity in the cabin air will require that all of the cooled air be passed through the filter 36.
Combining with the main flow of air in the duct II, the cooled and humidity regulated air, modulates the temperature and humidity of the entire volume of the air flowing into the cabin, whereby 0 the temperature and humidity of the air in the cabin are maintained within a predetermined range of values.
I claim as my invention:
1. In a cabin air conditioning system of the character described, the combination of: means for recirculating a main flow'of cabin air; means for diverting and compresing a part of said main flow of air; a cooling means; means for passing the diverted compressed air through said cooling means to cool the same; means for reexpanding and further cooling the compressed, cooled air; means for removing moisture from only a part of the reexpanded air; and means for delivering said part of the air back into said main flow of air. I
2. In a cabin air conditioning system of the character described, the combination of: means for recirculating a main flow of cabin air; means for diverting and compressing a part of said main flow of air; a cooling means; means for passing the diverted compressed air through said cooling means to cool the same; means for reexpanding and further cooling the compressed, cooled air; and a humidity control unit receiving the reexpanded and cooled air, said unit having two paths of flow for the air leading back into said mainflow of air, one of said paths of flow having moisture removing means therein, and a proportioning valve for directing said reexpanded air through said paths of flow, and means responsive to the humidity of the cabin air for controlling said valve, whereby moisture will be'removed from only a portion of said reexpanded air in accordance with the deviation acaaaaa scribed range.
3; In a cabin air conditioning system of the I character described, the combination of: means for recirculating a main now of cabin air; means for diverting and compressing a\part of said main flow of air; a cooling mea'ns; means for passing the' diverted compressed air through said cooling means to cool the same; mean for reexpanding and further cooling the compressed, cooled air; means operating in response to changes in temperature of the cabin air for controlling the action of said cooling means; means for removing moisture from only apart of the reexpanded air; and means for delivering said part of the air back into-said main flow of air.
4. In a cabin air conditioning system of the character described, the combination of: means for recirculating a main flow of cabin air; means for diverting and compressing a part of said main flow of air; a cooling means; means for passing the diverted compressed air through said cooling means to cool the same; means operating in response to changes in temperature of the cabin air for controlling the action of said cooling means; means for reexpanding and further cooling the compressed, cooled air; and a humidity control unit receiving the reexpanded and cooled air, said unit having two paths of flow for the air leading back into said main flow of air, one of said paths of flow having moisture removing means therein, and a proportioning valve for directing said reexpanded air through said paths of flow, and means responsive to the humidity of the cabin air for controlling said valve, whereby moisture will be removed from only a portion of said reexpanded air in accordance with the deviation of the humidity of the cabin air from a prescribed range.
5. In a cabin air conditioning-system of the character described, the combination of: means for recirculating a main flow of cabin air; means for diverting and compressing a part of said main flow of air; a cooling means; means for passing the diverted compressed air through said cooling means to cool the same; means operating in response to changes in temperature of the cabin air for controlling the action of said cooling means; means for reexpanding and fur ther cooling the compressed, cooled air; and a humidity control unit receiving the reexpanded and cooled air, said unit having two paths of fiow for the air leading back into said main flow.
of air, one of said paths of flow having moisture removing means therein, a proportioning valve for directing said reexpanded air through said paths of flow, and means responding to changes in the humidity of the cabin air for adjusting the position of said proportioning valve, whereby moisture will be removed from only a portion of said reexpanded air in accordance with the deviation of the humidity of the cabin air from a prescribed range.
6. In a cabin air conditioning system of the character described, the combination of means for recirculating a main flow of cabin air; means for diverting and compressing a part of said main flow of air; a cooling means; means for passing the diverted compressed air through said cooling means to cool the same; means for reexpanding and further cooling the compressed, cooled air; and a humidity control unit receiving the reexpanded and cooled air, said unit having two paths of new for the air leading back into said main flow of air, one of said paths of flow having moisture removing means therein,
flowstraightening means, at least in the outlet I part of said unit, and a proportioning valve for directing said reexpanded air through said paths of flow, and means responsive to the humidity of the cabin air for controlling said valve, whereby moisture will be removed from only a portion of said reexpanded air in accordance with the deviation of the humidity of the cabin'air' from a prescribed range.
'7. In a cabin air conditioning system having means for circulatingair, the combination of: means for passing a first flow of air into the cabin; means for compressing a second flow of air; a cooling means;- means for passing the compressed air through said cooling means to cool the same; means for reexpanding and further cooling the compressed, cooled air; means for removing moisture from only a part of the reexpanded air; and means for delivering said second flow of air into said first fiow of air.
8. In a cabin air conditioning system of the character described, the combination of means for passing a main flow of air into the cabin; means or ompressing a second flow of air; a cooling means; means for passing the compressed air through said cooling means to cool the same;
means for reexpanding and further cooling the compressed, cooled air; and a humidity control unit receiving the reexpanded and cooled air, said unit having two paths of flow for the air leading into said main flow of air, one of said paths of flow having moisture removing means therein, and a proportioning valve for directing said reexpanded air through said paths of flow,
a humidostat for controlling said valve, whereby 9. In a cabin air conditioning system of the character described, the combination of means for passing a main flow of air into the cabin; means for compressing a second fiow of air; a cooling means; means for passing the compressed air through said coolin means to cool the same;
means for reexpanding and further cooling the compressed, cooled air; and a humidity control unit receiving the reexpanded and cooled air, said unit having two paths of flow for the air leading into said main flow of air, one of said paths of flow having moisture removing means therein, a
proportioning valve for directing said reexpanded air through said paths of flow, and means responding to changes in the humidity of the cabin air for adjusting the position of said proportioning valve, whereby moisture will be removed from only a portion of said reexpanded air in accordance with the deviation of the humidity of the cabin air from a prescribed range.
10. In a cabin air conditioning system of the -character described, the combination of means paths of flow for the air leading into said main flow of air, one of said paths of flow having moisture removing means therein, and a proportioning valve for directing said reexpanded air through said paths of flow, and means responsive to the humidity of the cabin air for controlling said valve, whereby moisture will be removed from only a portion of said reexpanded air in accordance with the deviation of the humidity of the cabin air from a prescribed range.
11. In a cabin air conditioning system of the character described, the combination of: means for passing a flow of air into the cabin; means for compressing said flow of air; a cooling means; means for passing the compressed air through said cooling means to cool the same; means for reexpanding and further cooling the compressed cooled air; and a humidity contro1 unit receiv-; ing the reexpanded and cooled air, said unit having two paths of flow for the air leading toward the cabin, one of said paths of flow having mois ture removing means therein, a proportioning valve for directing said reexpanded air through said paths of flow, and means responding to changes in the humidity of the cabin air for adjusting the position of said proportioning valve, whereby moisture will be removed from only a portion of said reexpanded air in accordance with the deviations of the humidity of the cabin air from a prescribed range.
12. In a cabin air conditioning system of the character described, the'combination of: means for passing a flow of air into the cabin; means for compressing said flow of air; a cooling means; means for passing the compressed air through said cooling means to cool the same; means operating in response to changes in temperature of the cabin air for controlling the action of said cooling means; means for reexpanding and fur- .ther cooling the compressed cooled air; and a humidity control unit receiving the reexpanded and cooled air, said unit having two paths of HOW for the air leading toward the cabin, one of said paths of flow having moisture removing means therein, a proportioning valve for directing said reexpanded air through said paths or flow. and means responding to changes in th humidit of the cabin air for adjusting the position or said proportioning valve, whereby moisture will be removed from only a portion of said reexpanded air in accordance with the deviations of the humidity of the cabin air from a prescribed range.
13. In a cabin air conditioning system having means for circulating air, the combination of: means for passing a flow or air into the cabin; means for compressing said flow of air; a cooling means; means for passing said compressed air through said cooling means to cool the same; means for reexpanding and further cooling the compressed cooled air; a humidity control unit receiving the reexpanded and cooled air, said unit havin two paths of flow for the air leading toward the cabin, one ofsaid paths of now having moisture removing means therein; a proportioning valve for directing said reexpanded air through said paths of flow; and means responding to changes in the humidity of the cabin air for adjusting the position of said proportioning valve, said air compressing means, cooling means,
4 reexpanding means and humidity control unit being arranged in series.
SOREN K. ANDERSEN.
REFERENCES CITED The following references are of record in the file of this patent:
US614323A 1945-09-04 1945-09-04 Humidity control in aircraft air conditioning Expired - Lifetime US2485522A (en)

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US2566617A (en) * 1949-10-28 1951-09-04 Vapor Heating Corp Aircraft refrigeration control
US2585570A (en) * 1946-07-29 1952-02-12 Lockheed Aircraft Corp Aircraft pressurizing and cooling system
US2614815A (en) * 1947-01-20 1952-10-21 Bristol Aeroplane Co Ltd Aircraft cabin pressurizing and air conditioning apparatus
US2800002A (en) * 1954-02-02 1957-07-23 Garrett Corp Cabin refrigeration system
US2867989A (en) * 1955-02-17 1959-01-13 United Aircraft Corp Water separator de-icing control
US2943460A (en) * 1955-07-05 1960-07-05 North American Aviation Inc Ice prevention in air conditioning systems
US2959025A (en) * 1957-07-16 1960-11-08 Union Stock Yard & Transit Co Chicago Household refrigerator
US2992542A (en) * 1956-10-23 1961-07-18 Garrett Corp Ice formation control for air conditioning systems
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US3226946A (en) * 1963-01-24 1966-01-04 Normalair Ltd Air conditioning systems for aircraft
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US3878692A (en) * 1974-04-22 1975-04-22 Garrett Corp Aircraft cabin cooling method and apparatus
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US4263786A (en) * 1979-07-10 1981-04-28 The Boeing Company Fuel conserving air-conditioning apparatus and method for aircraft
US4461155A (en) * 1979-09-10 1984-07-24 Bertil Werjefelt Aircraft cabin ventilation system
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US5050109A (en) * 1989-12-19 1991-09-17 The Boeing Company Method and apparatus for measuring the humidity of ambient air surrounding an aircraft in flight
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US5555745A (en) * 1995-04-05 1996-09-17 Rotoflow Corporation Refrigeration system
US20100273410A1 (en) * 2006-03-29 2010-10-28 Airbus Deutschland Gmbh Device And Method For Distributing Air In A Cargo Aircraft
US20100327592A1 (en) * 2008-01-23 2010-12-30 Michael Boot Air-inlet system for internal combustion engine, air-conditioning system and combustion engine comprising the air-inlet system
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Cited By (26)

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Publication number Priority date Publication date Assignee Title
US2585570A (en) * 1946-07-29 1952-02-12 Lockheed Aircraft Corp Aircraft pressurizing and cooling system
US2614815A (en) * 1947-01-20 1952-10-21 Bristol Aeroplane Co Ltd Aircraft cabin pressurizing and air conditioning apparatus
US2566617A (en) * 1949-10-28 1951-09-04 Vapor Heating Corp Aircraft refrigeration control
US2800002A (en) * 1954-02-02 1957-07-23 Garrett Corp Cabin refrigeration system
US2867989A (en) * 1955-02-17 1959-01-13 United Aircraft Corp Water separator de-icing control
US2943460A (en) * 1955-07-05 1960-07-05 North American Aviation Inc Ice prevention in air conditioning systems
US2992542A (en) * 1956-10-23 1961-07-18 Garrett Corp Ice formation control for air conditioning systems
US3016623A (en) * 1956-11-13 1962-01-16 Cleveland Pneumatic Ind Inc Transport vehicle
US2959025A (en) * 1957-07-16 1960-11-08 Union Stock Yard & Transit Co Chicago Household refrigerator
US3226946A (en) * 1963-01-24 1966-01-04 Normalair Ltd Air conditioning systems for aircraft
US3326109A (en) * 1964-03-11 1967-06-20 Bristol Siddeley Engines Ltd Air conditioning systems for aircraft
US3878692A (en) * 1974-04-22 1975-04-22 Garrett Corp Aircraft cabin cooling method and apparatus
US4263786A (en) * 1979-07-10 1981-04-28 The Boeing Company Fuel conserving air-conditioning apparatus and method for aircraft
WO1981000757A1 (en) * 1979-09-10 1981-03-19 B Werjefelt Aircraft cabin ventilation system
US4461155A (en) * 1979-09-10 1984-07-24 Bertil Werjefelt Aircraft cabin ventilation system
US4523517A (en) * 1980-09-02 1985-06-18 Lockhead Corporation All electric environmental control system for advanced transport aircraft
US5050109A (en) * 1989-12-19 1991-09-17 The Boeing Company Method and apparatus for measuring the humidity of ambient air surrounding an aircraft in flight
US5086622A (en) * 1990-08-17 1992-02-11 United Technologies Corporation Environmental control system condensing cycle
US5555745A (en) * 1995-04-05 1996-09-17 Rotoflow Corporation Refrigeration system
WO1996031744A1 (en) * 1995-04-05 1996-10-10 Rotoflow Corporation Refrigeration system
US20100273410A1 (en) * 2006-03-29 2010-10-28 Airbus Deutschland Gmbh Device And Method For Distributing Air In A Cargo Aircraft
US9242734B2 (en) * 2006-03-29 2016-01-26 Airbus Deutschland Gmbh Device and method for distributing air in a cargo aircraft
US20100327592A1 (en) * 2008-01-23 2010-12-30 Michael Boot Air-inlet system for internal combustion engine, air-conditioning system and combustion engine comprising the air-inlet system
EP3130863A4 (en) * 2014-09-23 2017-12-27 Commercial Aircraft Corporation Of China Ltd Dewatering device for air conditioning system in aircraft
US10773809B2 (en) 2014-09-23 2020-09-15 Commercial Aircraft Corporation Of China, Ltd Dewatering device for an air conditioning system of a plane
DE102015200111A1 (en) * 2015-01-08 2016-07-14 Airbus Operations Gmbh Cooling system with a water separator and method of operating a cooling system

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